Bethel

After making a refueling stop, the pilot took off at night and was cruising at FL200. After about 30 minutes of flight, the right engine fuel filter bypass warning light illuminated. About 2 minutes later, the same warning light for the left engine illuminated. Soon thereafter the right engine, then the left engine, lost power. The pilot made a forced landing on a moving ice pack in the Bering sea, which resulted in substantial damage. Ice was found in the engine and main fuel screens. Significant amounts of water and/or ice were found in 3 tanks, which had been refueled before takeoff. A higher than normal amount of water was also found in the fuel sample taken from the nozzle of the refueling tanker. The flight manual required that an approved ice inhibitor be added to the fuel, if not premixed. Fuel at the refueling stop was not premixed and the pilot had no icing inhibitor (prist) with him on this flight. He did not drain fuel from the tanks during preflight, since the temperature was so cold he feared the drain might freeze open.

The airplane rolled 200-300 feet before becoming airborne in a very nose high attitude. It maintained this attitude, made a right, then a left bank, and fell to the ground in a nose high attitude. The cargo consisted of eight 55-gallons drums of fuel, laid on their side and secured by one cargo strap running fore and aft and another cargo strap running diagonally across the barrels. The tie down ring ultimate strength rating was 1,600 pounds. The weight of the cargo was 2,863 pounds. Three of the cargo hooks associated with the cargo straps were found still attached to the tie down rings, and one hook and tie down ring were not located. Post-impact fire destroyed the cargo straps, and the barrels were strewn randomly through the cabin/cargo area. According to the manufacturer, the davis tie down ring installation is not approved by the manufacturer. The modification should have been accomplished under a supplemental type certificate. The logbooks showed only an entry. The certificated max gross weight was calculated to have been exceeded by 324.8 lbs. The pilot, sole on board, was killed.

The non-scheduled, all cargo, air taxi flight was landing at the mining strip and upon touchdown the pilot-in-command released the yoke with his left hand and grabbed the nose steering tiller. The pilot-in-command stated that before he could apply reverse thrust, the nose of the airplane came up off the ground and the airplane began to veer to the right. He applied left rudder and power to the right engine, but the airplane left the right side of the runway.

The aircraft was destroyed when the aircraft struck a 350 foot high hill along its route. This flight was a part 135 on-demand air taxi cargo flight. Several other air taxi operators and company aircraft elected to cancel their flights. Both ground reports and pilot reports stated the weather in the area of the accident was ceilings below 500 feet and visibility less than one mile. The pilot, sole on board, was killed.

A total loss of power was experienced on takeoff due to the fuel selector being in the off position. The pilot attempted to restart the engine during which time the aircraft entered a stall and collided with the terrain. According to passengers the pilot did not use a checklist nor where the passengers briefed before the flight. The wreckage was visible from the airport control tower but was not located until several hours after the accident by air search. Two passengers were seriously injured while a third passenger and the pilot were killed.

En route from Bethel to Holy Cross, the pilot encountered technical problems with the engine that oversped and failed. He reduced his altitude and completed an emergency landing in Paimiut. The pilot escaped uninjured while the airplane was damaged beyond repair.

While taking off at Napaskiak Airfield, the engine failed. The aircraft crash landed, struck a drainage ditch and came to rest. All seven occupants escaped uninjured or with minor injuries and the aircraft was damaged beyond repair.

After takeoff from Bethel, en route to Kuskokwim River, the crew encountered an unexpected situation and elected to return. On final, the airplane went out of control and crashed. Both pilots were killed.

While cruising in poor weather conditions (whiteout conditions) on a cargo flight from Bethel to Tununak, the single engine airplane struck the ground and crashed. The pilot, sole on board, was killed.

On approach to Toksook Bay Airport, the crew encountered whiteout conditions with fog and snow falls. While descending under VFR mode, the crew failed to realize his altitude was too low when the airplane struck the ground and crashed in a snow covered area located short of runway. Both crew members were injured and the aircraft was destroyed.